MS-500V

The engines are intended for installation in various-purpose helicopters with takeoff mass of 3.5 to 6 t and permit to attain high economic standards in the course of commercial use.

Main advantages of the engine:

simple and effective design;
high reliability;
low specific fuel consumption;
high stability of characteristics in service;
compliance with current and future environmental requirements;
extended service life and durable calendar life;
ease and convenience of maintenance and repair;
low cost of life cycle.

Basic specifications:

Engine MS-500V MS-500V-01 MS-500V-02

With one engine inoperative (OEI) (SLS, ISA):

2,0-min power; hp (kW)
(flat-rated to t_AMB, °C) 1000 (735)
(+15) 1200 (883)
(+30)

2,5-min power; hp (kW)
(flat-rated to t_AMB, °C) 710 (522)
(+15) 900 (662)
(+25) 1100 (809)
(+35)

30,0-min power; hp (kW)
(flat-rated to t_AMB, °C) 659 (485)
(+25) 850 (625)
(+30) 1000 (735)
(+30)

Take-off power rating (SLS, ISA):

Power, hp (kW)
(flat-rated to tAMB, °C) 630 (463)
(+35) 810 (595)
(+35) 950 (699)
(+30)

Óäåëüíûé ðàñõîä òîïëèâà, êã/ë.ñ.·÷ (êã/êÂò·÷) 0.260 (0.354) 0.239 (0.325) 0.230 (0.313)

Cruise power rating (SLS, ISA)

Power, hp (kW)
(flat-rated to t_AMB, °C) 450(331)
(+45) 450(331)
(+35) 500(368)
(+35)

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Applicability

Aircraft engines

Industrial installations

Consumer goods

Services